Chinese translation for "姿态机动"
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- attitude manoeuvre
Related Translations:
俯冲姿态: diving attitudediving position 姿态稳定: attitude dampingattitude holdattitude stabilization 姿态计算: attitud computation 巡航姿态: cruise attitudecruise position 姿态监控: attitude monitoring 姿态校正: attitude correctionattitude updatingattitudecorrection 姿态指示: attitude indication
- Example Sentences:
| 1. | Vibration reduction of attitude control for flexible spacecraft
挠性飞行器姿态机动的振动抑制 | | 2. | Active vibration control of flexible spacecraft during attitude maneuver
挠性航天器姿态机动的主动振动控制 | | 3. | Hardware - in - the - loop for small satellite model independent large angle attitude maneuver
小卫星模型独立大角度姿态机动半实物仿真 | | 4. | Abstract : large angle manetwer control technique is imporlont for the small satellite , this paper discussed the mstoataneous - turn - axis control arithmetic
文摘:大角度姿态机动控制技术是高分辨率遥感小卫星的关键技术之一。 | | 5. | The input - output linearization control is combined with the adaptive fuzzy sliding mode control , and is applied to the attitude maneuver control of the flexible satellite
摘要将输入输出线性化控制与自适应模糊滑模控制相结合，并将其应用于挠性卫星姿态机动控制中。 | | 6. | At last , simulations are presented . 3 . based on the attitude control of the flexible spacecraft , this paper prompts a method to change nonlinear state equations to t - s fuzzy model
论文研究的目的是,挠性航天器在平面内作大角度姿态机动时,实现对柔性帆板振动的控制。 | | 7. | Through it the author made a deep study of the satellite attitude control subsystem , verified several sorts of disturbance torques and realized satellite three - axis attitude stabilization control and attitude maneuver under different conditions
本文在simulink下对卫星姿控系统作了比较深入的研究，对各种干扰力矩进行了验证，同时在不同的仿真条件下实现了卫星三轴稳定控制、姿态机动和飞轮的磁卸载。 | | 8. | In addition , the principle of component synthesis vibration suppressing ( csvs ) method is also briefly introduced and summarized to several lemmas , which can suppress flexible vibration by utilizing the character of vibration system itself and has the characters of simple , multiform , easy to apply and so on
另外,为了将分力合成方法应用于挠性系统的振动抑制,简要地介绍了分力合成方法的一些基本概念及原理。针对采用推力器作为执行机构的挠性航天器姿态机动的振动抑制问题,提出了将分力合成振动抑制( csvs )方法和基于分布压电元件( pzt )的主动振动抑制技术相结合的一种复合主动控制方法。 | | 9. | About the large deformation description , a multi - floating coordinate system is adopted . it can effectively reduce the error of discretization . this paper deals with the design of restrained variable structure control in the way of phase plane analyse , which is concise and avoids complex mathematical descriptions . a new method is promoted for flexible spacecraft control by describing flexible spacecraft dynamics equations as t - s fuzzy model and designing a pdc fuzzy controller
将挠性航天器姿态动力学方程描述为t - s模糊模型为挠性航天器控制提供了新思路;仿真结果表明,基于t - s模型的pdc模糊控制器能满足挠性航天器大角度姿态机动的精度要求,并能有效抑制帆板振动,具有一定的智能性。 |
- Similar Words：
- "姿态回转仪" Chinese translation, "姿态获取" Chinese translation, "姿态基准" Chinese translation, "姿态基准平台" Chinese translation, "姿态基准信号" Chinese translation, "姿态计算" Chinese translation, "姿态监控" Chinese translation, "姿态检查仪表组" Chinese translation, "姿态角" Chinese translation, "姿态角速度" Chinese translation
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